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a spherical spacecraft (diameter of 1m) has a transmissivity of 0.0 and reflectivity of 0.8 if...

a spherical spacecraft (diameter of 1m) has a transmissivity of 0.0 and reflectivity of 0.8 if the solar flux incident upon the spacecraft is 1370 w/m^2 what is the rate of incident energy absorbed by the spacecraft?

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50)- Rate of énery Absored Q4 As Cin 960-796-

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